• Title/Summary/Keyword: LIFTING LOAD COMPUTATION

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A computation model for Resource-based Lifting loads of the lift-cars for super high-rise buildings (초고층 건축물 리프트카 양중계획수립을 위한 자원기반의 양중부하 산정 모형)

  • Han, Choong-Hee;Lee, Jun-Bok;Won, Seo-Kyung
    • Korean Journal of Construction Engineering and Management
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    • v.13 no.5
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    • pp.135-143
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    • 2012
  • Constructing super-tall buildings is significantly different from constructing general ones in every technological and managerial aspects. Especially lift-car operations planning and management is one of core parts among various management techniques required during the course of the whole construction process of the super-tall buildings because vertical movements of physical resources enormously affect the efficiency of the construction processes. However, discrepancy between lifting plans and actual lifting operations causes serious efficiency problems. As an effort to solve the problem, this research suggests an improved method of estimating resource-based lifting load. The computing model developed as a result of this research facilitates more accurate computation of the total operation time and the maximum lifting capacity of the lift-cars. Further, this research can be developed as a decision support system for the total lift-car operations management.

Loose Coupling Approach of CFD with a Free-Wake Panel Method for Rotorcraft Applications

  • Lee, Jae-Won;Oh, Se-Jong;Yee, Kwan-Jung;Kim, Sang-Hun;Lee, Dong-Ho
    • International Journal of Aeronautical and Space Sciences
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    • v.8 no.1
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    • pp.1-9
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    • 2007
  • As a first step toward a complete CFD-CSD coupling for helicopter rotor load analysis, the present study attempts to loosely couple a CFD code with a source-double panel method. The far-field wake effects were calculated by a time-marching free vortex wake method and were implemented into the CFD module via field velocity approach. Unlike the lifting line method, the air loads correction process is not trivial for the source-doublet panel method. The air loads correction process between the source-doublet method and CFD is newly suggested in this work and the computation results are validated against available data for well-known hovering flight conditions.